Plug-in composite power distribution assembly and system including same

A power distribution assembly (100) is provided for a system such as, for example, an aircraft electrical system (2). The power distribution assembly (100) includes a frame (102) having a number of mounting points (104,106,108,110) structured to be mounted to a thermally conductive structure such as...

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Bibliographic Details
Main Authors MCCORMICK JAMES MICHAEL, MILLS PATRICK WELLINGTON
Format Patent
LanguageChinese
English
Published 12.02.2014
Subjects
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Summary:A power distribution assembly (100) is provided for a system such as, for example, an aircraft electrical system (2). The power distribution assembly (100) includes a frame (102) having a number of mounting points (104,106,108,110) structured to be mounted to a thermally conductive structure such as, for example, an aircraft panel (200). A shell (120) is disposed on the frame (102). A backplane (130) is disposed within the shell (120). The backplane (130) includes a plurality of at least partially embedded electrical conductors (132,134,136,138,140,142,144,146,148,150,152). Electrical apparatus (154,156,158,160,162) such as, for example, relays or contactors (154,156,158), are electrically connected to the at least partially embedded electrical conductors (132,134,136,138,140,142,144,146,148,150,152). The relays or contactors (154,156,158) generate heat. The backplane (130), the at least partially embedded electrical conductors (132,134,136,138,140,142,144,146,148,150,152), and the frame (102) provide a direc
Bibliography:Application Number: CN201280026682